TY - JOUR
T1 - Thermal characterization of epoxy bilayer hybrid composites reinforced with kenaf and oil palm fibers
AU - Hanan, Farah
AU - Khan, Tabrej
AU - Jawaid, Mohammad
AU - Sultan, Mohamed Thariq Hameed
AU - Sebaey, Tamer
AU - Singh, Balbir
AU - Sarmin, Siti Noorbaini
N1 - Funding Information:
The authors are thankful to the Ministry of Higher Education, Govt. of Malaysia for Providing Higher Institution Centre of Excellence Grant No: 6369108 for conducting this research work.
Funding Information:
The authors are thankful to the Ministry of Higher Education, Govt. of Malaysia for Providing Higher Institution Centre of Excellence Grant No: 6369108 for conducting this research work.
Publisher Copyright:
© 2022 Society of Plastics Engineers.
PY - 2023/1
Y1 - 2023/1
N2 - Natural fiber-based materials are widely accepted in the composite sector as a substitute for synthetic fiber, particularly in structural and semi-structural implementations in the automotive and aerospace industries, reflecting a recent trend and increased awareness of the importance of sustainable product design. Hand lay-up was used to create natural fiber bilayer hybrid composites with epoxy matrix reinforcing oil palm empty fruit bunch (EFB) and kenaf fiber matting. The overall effect of this hybridization of the natural fiber and the thermal characterizations were studied experimentally. Both the hybrid combinations kenaf fiber and oil palm EFB were made by maintaining the fiber loading at 50% (weight) and weight ratios at 1:1, 1:4 and 4:1. The Tan delta, loss modulus (E″), storage modulus (E′), and Cole-Cole plot were found to be useful in investigating dynamic mechanical properties. Dynamic mechanical analysis results like coefficient of performance and Cole-Cole plot clearly show that hybrid pure kenaf composite has the significant complex modulus because interfacial bond between fiber and matrix is strong. As a result, it has been determined that kenaf fibers have the best mixing ratio for improving the dynamic mechanical properties of these hybrid type composites and can be used for aerospace, automotive, and civil engineering applications requiring high dimensional stability and excellent mechanical properties. The thermal gravimetric analysis data demonstrated that as compared to pure, the kenaf fibers and hybrid oil palm empty fruit bunch composites have the best thermal stability, with the highest beginning and ultimate breakdown temperatures of 200 and 450°C, respectively.
AB - Natural fiber-based materials are widely accepted in the composite sector as a substitute for synthetic fiber, particularly in structural and semi-structural implementations in the automotive and aerospace industries, reflecting a recent trend and increased awareness of the importance of sustainable product design. Hand lay-up was used to create natural fiber bilayer hybrid composites with epoxy matrix reinforcing oil palm empty fruit bunch (EFB) and kenaf fiber matting. The overall effect of this hybridization of the natural fiber and the thermal characterizations were studied experimentally. Both the hybrid combinations kenaf fiber and oil palm EFB were made by maintaining the fiber loading at 50% (weight) and weight ratios at 1:1, 1:4 and 4:1. The Tan delta, loss modulus (E″), storage modulus (E′), and Cole-Cole plot were found to be useful in investigating dynamic mechanical properties. Dynamic mechanical analysis results like coefficient of performance and Cole-Cole plot clearly show that hybrid pure kenaf composite has the significant complex modulus because interfacial bond between fiber and matrix is strong. As a result, it has been determined that kenaf fibers have the best mixing ratio for improving the dynamic mechanical properties of these hybrid type composites and can be used for aerospace, automotive, and civil engineering applications requiring high dimensional stability and excellent mechanical properties. The thermal gravimetric analysis data demonstrated that as compared to pure, the kenaf fibers and hybrid oil palm empty fruit bunch composites have the best thermal stability, with the highest beginning and ultimate breakdown temperatures of 200 and 450°C, respectively.
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U2 - 10.1002/pc.27108
DO - 10.1002/pc.27108
M3 - Article
AN - SCOPUS:85139968760
SN - 0272-8397
VL - 44
SP - 444
EP - 452
JO - Polymer Composites
JF - Polymer Composites
IS - 1
ER -